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Table of Tasks Chapter 5 Chapter 2 Change Map Orientation ..................5-6 Switch to the PFD Operating Mode ..............2-4 Switch Back to MFD Operating Mode ..............2-4 Changing Feature Group Display Setting ............5-10 Chapter 4 Change the Map Range ..................5-11 View Database Validity and Expiration Dates ..........4-3 Turn Auto Range Off or On ...................5-12 Activate Auto-Range ....................5-12 Viewing PAGES .........................4-5...
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Hide the METAR Legend ..................5-34 Display WX-500 Cells ....................5-67 Display Multiple Airports’ METAR Information ..........5-35 Clear WX-500 Rate ......................5-67 Display an Individual Airport’s METAR Information .......5-36 Activate WX-500 Self-Test ..................5-67 Display the Echo Tops Legend ................5-37 Modify the Course Setting ..................5-71 Chapter 6 Hide the Echo Tops Legend .................5-37 Increase or Decrease Echo Top Altitude Filter ...........5-38...
Copyright 2007-2009. The Aspen Avionics EFD1000/500 MFD provides access to information from multiple sources. Aspen Avionics does not control, edit or review Aspen Avionics® is a registered trademark of Aspen Avionics, Inc. the content of said information and as such, is not responsible for Evolution™, EFD1000 Pro PFD™, EFD1000 MFD™, EFD500 MFD™,...
Display (EFD500 MFD). This guide is current as of the Date Published. Specifications and operational details are subject to change without notice. Please visit the Aspen Avionics web site, aspenavionics.com, for the most up-to-date Pilot’s Guide. Installation of the EFD1000/500 MFD in a type-certificated aircraft...
LIMITED WARRANTY Aspen Avionics, Inc. 1. YOUR WARRANTY. Aspen Avionics, Inc. (“Aspen”) warrants to Furnish proof sufficient to establish that the item is a you, the original purchaser, that its Products (if purchased from an Nonconforming Product, and authorized dealer) will comply with applicable specifications (as set Allow Aspen access to all relevant records in order to forth in the owner’s manual) in all material respects and will be free...
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Accident, contamination, damage from a foreign object or 8. EXCLUSIVE WARRANTY. THIS WARRANTY IS EXCLUSIVE AND weather conditions, abuse, misuse, neglect, or negligence, IN LIEU OF ALL OTHER WARRANTIES. THE IMPLIED WARRANTY OF MERCHANTABILITY AND IMPLIED WARRANTY OF FITNESS FOR A Exposure of the product or the product’s host medium to any PARTICULAR PURPOSE, AS WELL AS ALL OTHER IMPLIED WARRANTIES computer virus or other intentionally disruptive, destructive,...
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Aspen Customer Service at (505) 856-5034; by offered by a dealer (“Dealer Warranty”) will be the sole responsibility writing to Aspen Customer Service Department, Aspen Avionics, Inc., of the dealer, who will be solely responsible for all liability, loss, cost, 5001 Indian School Road NE, Albuquerque, New Mexico, 87110;...
Weather Data Warranty LIMITS ON OUR RESPONSIbILITY THE WEATHER DATA SOFTWARE PRODUCT IS PROVIDED “AS IS. ” ALL OTHER WARRANTIES, EXPRESSED OR IMPLIED, INCLUDING ANY WARRANTY OF DISCLAIMERS. EXCEPT AS EXPRESSLY PROVIDED HEREIN, MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE OR OF NON- WE MAKE NO WARRANTY OR REPRESENTATION, EITHER INFRINGEMENT ARE HEREBY EXCLUDED.
XM WX Satellite Radio Service Agreement Hardware and required monthly subscription sold separately. Subscription fee is consumer only. Other fees and taxes, including a one-time activation fee may apply. All programming fees and weather data are subject to change. XM WX weather data displays and individual product availability vary by hardware equipment.
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This guide covers all the functionality available in the EFD1000 MFD and EFD500 MFD. The EFD500 MFD does not include an AHRS and ADC sensor, Secondary HSI, and does not support Reversionary mode. See Aspen Avionics document number 091-00005-001 EFD1000 PFD Pilot’ s Guide for complete instructions on the EFD1000 PFD.
Term Definition NOTE A VIEW is the graphical content of a WINDOW. The VIEW presents specific The Secondary AI and HSI VIEWS do not display a information such as terrain, traffic, or weather. A VIEW is the same size as the name label.
Pilot Interface Modes The EFD1000/500 MFD has several interface modes described in Table 2. The current mode determines the functionality of the content-sensitive pilot controls. Term Definition When the EFD1000/500 MFD first initializes it is in PAGE (and VIEW) Selection mode. Rotating the Left Knob selects different PAGES. When PAGE PAGE Selection mode is active the Pg #/3 label above the Left Knob is magenta in color (# indicates the current page number).
Color Philosophy Table 3 provides an overview of the color convention used on the EFD1000/500 MFD display. NOTE As the number of colors used on the display is limited, to ensure adequate color differentiation under all lighting conditions. There are a few cases where a given color is used in a slightly different context than described in the following table.
Warnings, Cautions, and Notes Where applicable; warnings, cautions, and notes are given. Aspen Avionics uses the icons and definitions described in Table 4. Icon Definition Emphasizes a crucial operating or maintenance procedure, which, if not strictly observed, could result in injury to, or death of, personnel or long Warning term health hazards.
While the EFD1000 is reasonably intuitive and easy to use, some familiarity with Electronic Flight Instrument Systems (EFIS) and Horizontal Situation Indicators (HSI) is required. Aspen Avionics strongly recommends that new users of the EFD1000 get some dual instruction from an experienced instrument CFI, and spend some time becoming familiar with the PFD in day VFR conditions with a safety pilot, before flying in actual instrument meteorological conditions (IMC).
Chapter 1 Welcome & Introduction Welcome to Aspen Avionics’ Evolution Flight Display (EFD) system, the most flexible, expandable, and upgradable Electronic Flight Instrument System (EFIS) available for General Aviation aircraft. The EFD system is designed to replace traditional, mechanical primary flight instruments—...
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Pilot, Pro and ATP—each with increasing levels of features and capabilities, and each lower model is upgradable through software to the more capable models. For detailed information on the PFD see Aspen Avionics document number 091-00005-001 EFD1000 PFD Pilot’ s Guide.
You can even add another MFD, an EFD500 to round out a complete “six-pack” replacement and gain even more capability and flexibility (Figure 1-4). When you are ready to upgrade, simply contact an Aspen Avionics Authorized Dealer for more information.
1.1. System Hardware Depending on the EFD configuration you have selected, you will have some, all or NOTE several of the following pieces of hardware installed in your aircraft. The EFD1000 MFD system typically consists of the following pieces of hardware: The EFD1000 MFD comes standard without emergency • EFD1000 display unit GPS.
1.1.1. EFD1000 Display Pitot & Static System Connections (EFD1000 MFD) The EFD1000/500 display unit is a digital system that consists of a high resolution six-inch diagonal color LCD display, pilot controls, photocell, and microSD data card slot. The EFD display mounts to the front surface of most instrument panels. The following controls are present on the EFD1000/500 display bezel: • Reversionary / Power Button (REV) 44-pin D-Sub for Electrical Connections...
1.1.2. EFD500 Display The EFD500 MFD display is similar to the EFD1000 MFD display, but excludes the ADAHRS, Secondary HSI, and backup battery. The EFD500 can only be used as a Multi- Function Display (MFD). 1.1.3. Remote Sensor Module (RSM) (EFD1000 MFD only) The Remote Sensor Module (RSM) is an integral part of the EFD1000 system, and works together with the display unit sensors as part of the ADAHRS.
1.1.4. Configuration Module (CM) The Configuration Module contains an EEPROM device that retains system configuration and calibration data and provides two primary functions (Figure 1-7): • Retains aircraft-specific configuration information, calibration data, and pilot settings, allowing the PFD to be swapped for service purposes without re-entering Figure 1-7 or re-calibrating the installation.
1.1.6. Evolution Weather Receiver (EWR50) NOTE and Antenna - Optional A single receiver will supply data to all EFD units The optional Evolution Weather Receiver (EWR50) provides the ability to receive XM WX installed on the aircraft. Satellite Weather data with a paid subscription to XM WX Satellite Weather. The EWR50 consists of a receiver and antenna.
Chapter 2 MFD Overview This Pilot’ s Guide covers the EFD1000 and EFD500 MFD models. These NOTE systems are powerfully flexible and can be configured in a variety of ways, depending on the other aircraft systems with which they are integrated. The EFD500 MFD does not support the display of the secondary attitude data or the reversionary mode.
2.2. XM WX Satellite Weather Figure 2-2 XM WX Satellite Weather Display on the The EFD1000/500 MFD supports XM WX Satellite Weather when the aircraft is EFD1000/500 MFD configured with an Aspen EWR50 weather receiver (Figure 2-2). You must also purchase a subscription to XM WX Satellite Weather.
2.4. Traffic The EFD1000/500 MFD will support Traffic Awareness (Figure 2-4) when your aircraft is Figure 2-4 Dedicated Traffic Display on equipped with at least one of the following traffic receivers: the EFD1000/500 MFD • Avidyne TAS 600/610/620 (TAS) • Bendix/King KMH 880 (TAS) • Bendix/King KTA 870 (TAS) • Garmin GTX 330 (TIS) • RYAN 9900BX (TAS)
2.6. Manual Reversionary Mode (EFD1000 MFD only) When the EFD1000 MFD is configured alongside a PFD, the MFD supports a reversionary mode. The reversionary mode is a feature that allows the MFD to revert to a fully functional (except for tone generation and autopilot) Primary Flight Display. The MFD mode is the default mode on power-up and the “REV”...
2.7. Secondary PFD Display The EFD1000/500 MFD and the EFD1000 PFD constantly communicate with each other. Figure 2-8 When communication with the PFD is lost, the MFD shall annunciate in amber CROSS MFD/PFD Communication Lost Annunciations LINK FAILURE above the current baro setting in the data bar (Figure 2-8). This message means that a failure has been detected in the intercommunications and barometric NOTE pressure setting synchronization may be inoperative..
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Chapter 3 Display & Controls In order to best familiarize you with the features available for the EFD1000/500 MFD this chapter offers a quick overview of the display and Pilot Controls. Figure 3-1 Actual view of EFD1000 MFD Display Unit 091-00006-001 REV B EFD1000/500 MFD Pilot’s Guide Page 3-1...
Reversion and Power Button Range Buttons Menu Button Hot Key/Menu Key 1 Hot Key/Menu Key 2 Hot Key/Menu Key 3 Hot Key/Menu Key 4 Hot Key/Menu Key 5 Right Control Knob Lower Right Button Lower Center Button Lower Left Button Left Control Knob Automatic Dimming Photocell microSDHC Card Slot...
3.1. Default Display The EFD1000/500 MFD offers three different display options as described in the following paragraphs. The default VIEWs and other settings can be changed at any time. Any changes made to the PAGE are automatically saved and displayed over the power cycle of the unit.
The second PAGE of the display is a two WINDOW, Split Screen LAYOUT, and the Left Knob label reads 2/3. The VFR Navigation Map VIEW is displayed in the top WINDOW NOTE with the Dedicated Terrain VIEW is displayed in the bottom WINDOW (Figure 3-6). The Split Screen LAYOUT does not allow the display of Table 3-2 lists the VIEWS that will display in each of the Split Screen LAYOUT the Navigation Map VIEW and the Data Link Weather...
The last PAGE of the display is a three WINDOW, Thumbnail LAYOUT, and the Left Knob NOTE label reads 3/3. The Secondary Attitude Indicator VIEW is displayed in the top left WINDOW, Dedicated Terrain VIEW in the top right WINDOW, and VFR Navigation Map If a sensor is not configured in the Installation Menu VIEW in the bottom WINDOW (Figure 3-7).
3.1.1. Data Bar Last Active Next Waypoint Waypoint Waypoint The Data Bar is a multi-purpose text area that displays the information about the current flight plan and other relevant flight information. The Data Bar is not editable. The first line of the Data Bar displays flight plan information (Figure 3-8): • Last flight plan waypoint Estimated Aircraft...
3.2. Controls Your EFD display is equipped with several pilot controls designed to simplify operation of your EFD system, minimize pilot workload, and reduce the time required to access functionality. Each display bezel has two dual rotary knobs with a push feature, three lower buttons, five context sensitive Hot Key buttons along the lower right, a MENU Button, RNG+/- Button, and a REV Button for reversion or manual power control.
When the INFO button is pressed rotating the Left Knob selects different objects on the Navigation Map (Airports/VORs) or METAR, AIRMET/SIGMET, and TFR weather pages. Pressing the Left Knob after the INFO button has been pressed will display the selected object’s textual information, when available.
3.2.1.5. Right Knob Pressing the Right Knob moves the FOCUS and selects different WINDOWS on a PAGE. When a WINDOW has FOCUS, rotating the Right Knob changes the VIEW of the WINDOW. If the Right Knob is not pushed (to activate WINDOW selection) the initial rotation of the Right Knob will activate the selection process, and continued rotation will select different WINDOWs.
3.2.2.3. Menu Button The MENU Button is used to activate or exit the Main Menu. The first time the Main Menu is accessed the GENERAL SETTINGS menu page displays; subsequently, the last viewed menu page will display. 3.2.2.4. Hot Keys/Menu Keys The five buttons along the lower right side of the EFD1000/500 MFD display offer either NOTE Hot Key functionality, to rapidly select a common command, or to select a menu option...
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Chapter 4 Getting Started If you already have an EFD1000 PFD, you will probably find your new EFD1000/500 MFD fairly easy to use. However, because of all the information available to view, many of the controls on the EFD display unit have different functionality.
4.1. Startup When the EFD1000/500 MFD initializes you are presented with the default PAGES pre-configured with what we thought would be the most useful VIEWS. This section will give you a quick overview of the default settings so that you can start flying with the EFD1000/500 MFD right away.
View Database Validity and Expiration Dates Figure 4-2 EFD1000/500 MFD Database Access the Main Menu. Confirmation Screen Navigate to the Database page. The database expiration dates are displayed next to the database titles as shown in Figure 4-3. Push the MENU key to exit the Main Menu. CAUTION Terrain information is for awareness only.
4.1.1. Select Different PAGE or WINDOW Active Window As previously mentioned, a PAGE displays information on the EFD1000/500 MFD screen. When you make any changes to a PAGE, the PAGE settings are automatically updated and saved. Changes are made to the current PAGE by selecting the WINDOW and changing the VIEW or other options as desired.
Viewing PAGES Active Window • Rotate the Left Knob clockwise to select the next PAGE, counter-clockwise to select the previous PAGE. The label above the Left Knob will change to indicate the page number currently displayed (Figure 4-4 and 4-5). Selecting WINDOWS •...
4.1.2. Change VIEW Figure 4-8 Change VIEW – New VIEW Selected A WINDOW can display different VIEWs as outlined in Section 3.1. Default Display. To select a different VIEW in any WINDOW you must first move the FOCUS to the WINDOW you want to change, and then select a different VIEW.
4.1.3. Panning Figure 4-9 PUSH TO PAN Displays Above the Left Knob The Navigation Map and Data Link Weather VIEWs support a panning feature that allows the pilot to view areas away from the aircraft’s current position. Use the Panning Feature Select the WINDOW that contains the VIEW you want to pan.
4.1.4. Editing Airport Identifier Fields The METAR screen of the Data Link Weather VIEW allows the pilot to enter information by entering VIEW control mode and using the Data Field Edit functionality. For example, when looking for METAR information for a specific airport, the pilot can enter the airport identifier to display the required information.
Figure 4-15 NOTE METAR with Information Viewable by Scrolling The TEXT function is a smart function. It only selects a METAR capable airport rather than permitting selection of a random string of letters. Additionally, editing is done using only one hand — twist to the desired letter then press to advance. 4.1.5.
4.2. Main Menu The MENU Button is used to access the EFD1000/500 MFD’s Menu system to change options and also to change the EFD1000’s LCD brightness controls. 4.2.1. Using the Menus As previously discussed, you enter MENU mode by pressing the MENU Button. The Main MENU has several pages of information that allow the pilot to fully customize the EFD1000/500 MFD display.
is in Navigation mode, indicated by the magenta label SEL PAGE directly above the Right Knob (Figure 4-17). When in Navigation mode, rotating the Right Knob navigates through the menu pages. Rotate the Right Knob clockwise to advance to the next menu page.
The menu text will display in one of the four colors listed and described in Table 4-2. Figure 4-20 Main Menu Text - Editable DISPLAY DESCRIPTION DISPLAY TEXT Figure 4-21 Main Menu Text - Enabled WHITE See Figure 4-20 Editable option Figure 4-22 Main Menu Text –...
Edit Main Menu Items Figure 4-25 EDIT VALUE Displays Access the Main Menu. Above Right Knob Navigate to the desired menu page. Push the Menu Key of the desired option. The menu label turns magenta and the EDIT VALUE label displays above the Right Knob (Figure 4-25). Rotate the Right Knob to the desired value.
Display Lighting 4.3. Figure 4-26 EFD1000/500 MFD photocell The EFD1000/500 MFD contains various lighting controls to maintain readability under all lighting conditions. Each EFD1000/500 MFD has an LED backlight, which illuminates textual content for better night operation. The controls are also backlit, at a fixed brightness, for visual location in dark conditions.
Display Lighting MODE DESCRIPTION NOTE LCD backlight intensity is automatically adjusted based The AUTO display brightness setting is determined Automatic on the current light conditions sensed by the Automatic by the amount of light detected by the photocell AUTO Dimming Photocell. When using the auto-brightness the on the front of the unit.
4.4. Backup Battery The EFD units all have an internal backup battery in case of degraded external power. The internal battery provides sufficient power for 30 minutes of display operation at temperatures that would be comfortable to the aircraft occupants. The battery is charged by the EFD1000/500 MFD whenever the EFD unit is running on aircraft power.
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CAUTION WARNING During situations where a high electrical demand is placed on the When fully charged, the internal battery will operate the AHRS, display, aircraft electrical system, electrical transients that cause aircraft voltage and RSM emergency GPS for at least 30 minutes following loss of to momentarily drop below 12.5±0.3V (14V Electrical System) or aircraft power.
4.4.1. Power Override Figure 4-30 Main Menu, Power Settings, BATTERY and EXT PWR MENU Button Override the Automatic Power Configuration Push the MENU Button. The Main Menu displays. Rotate the Right Knob until the POWER SETTINGS Menu page displays. MENU Button 1 and 2 show the power source options of BATTERY and EXT PWR respectively.
4.5. Power Off/REV Button Figure 4-33 Main Menu, Power Settings, RESTART Menu Button The EFD1000/500 MFD is typically powered through a dedicated Power Control switch that is connected to the aircraft Battery bus. The system will power up, based on the position of the Power Control switch Like the PFD, the power for the EFD1000/500 MFD is normally routed through a switch on the main battery bus.
4.6. Range Button When the MAP is enabled, the RNG (Range) button is used to zoom in or out in scale to display more or less of the map. The map range available depends on the VIEW. Press the top or (+) of the RNG key to increase map range. Press the bottom or (–) of the RNG key to decrease map range.
Chapter 5 Reference Guide The EFD1000/500 MFD is a panel-mounted Electronic Flight Instrument NOTE System (EFIS) that presents the pilot with a full-color moving Navigation Map VIEW and a dedicated Terrain VIEW. Additionally there are three If the GPS becomes invalid an Invalid GPS optional VIEWS that provide Traffic, Stormscope®...
5.1. Navigation Map Figure 5-1 Navigation Map VIEW, IFR Style Map, Showing The Navigation Map VIEW is a pilot configurable, moving map. The Navigation Map Hot Key Menu 1/2 VIEW’s default map style is a VFR map, oriented North-Up with the Ownship symbol located at the center of rotation of the map displaying a 360°...
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The Range +/- button and the Map Hot Key allow the pilot to control the map range NOTE and provide feature declutter. The current map range and declutter settings are shown in the lower left corner of the VIEW. Additionally, more detailed customization Terrain and NEXRAD are mutually exclusive.
The data source for all but the active flight plan associated with the Navigation Map VIEW is obtained from the Jeppesen Database saved to the micro SD Card. If the Jeppesen Database is invalid or unavailable, DATABASE FAILURE is displayed in amber. While Navigation Map VIEW features (Table 5-2) are loading, a gray indicator displays on the bottom center of the Navigation Map VIEW.
5.1.1. General Map Settings There are several options available to customize the Navigation Map VIEW. The default settings for the Navigation Map VIEW are found in the Main Menu on the GENERAL SETTINGS page and two MAP SETTINGS pages . Based on your flying preferences you may want to change the Navigation Map orientation and other items you want to display.
Change Map Orientation Figure 5-3 Map General Settings Page Access the Main Menu. Navigate to the GENERAL SETTINGS menu page. Push the NAV MAP ORIENTATION Menu Key. The menu label turns magenta and the EDIT VALUE label displays above the Right Knob (Figure 5-3).
North-Up Heading-Up Track-Up • NORTH-UP label displays in the upper • HDG UP label displays in the upper right • TRK UP label displays in the upper right right corner of the VIEW. corner of the VIEW. corner of the VIEW. • Navigation Map VIEW is oriented North- • The aircraft heading is displayed in the • The aircraft ground track is displayed in...
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Feature Group & Layer Declutter Setting Order (top to bottom) Feature Max Range (nm) Traffic Symbols Overlay - enabled via TRFC Hot Key Ownship 2, 4 GPS Track Line 2, 4 Flight Plan Legs and 2000 Waypoints Obstructions Overlay – enabled via TERR Hot Key Limited to 40 but displayed to 2000 1, 3, 4 WX-500...
Changing Feature Group Display Setting Figure 5-4 Editing OTHER APTS Feature Access the Main Menu. Group Navigate to the MAP SETTINGS A or B page that lists the feature group you want to change. Push the Menu Key that corresponds to the name of the feature group you want to change.
5.1.3. Map Range Figure 5-6 Navigation Map VIEW at 15 nm Range The RNG +/- Button on the right of the EFD1000/500 MFD display is used to zoom in or out (respectively) to display more or less of the map. The pilot can select map ranges from 0.5 to 2000 nautical miles, incrementing one range value with each press of the RNG +/- button.
Turn Auto Range Off or On Figure 5-8 Map General Settings Page Access the Main Menu. Editing Auto Range Setting Navigate to the GENERAL SETTINGS menu page. Push the NAV MAP AUTO RNG Menu Key. The NAV MAP AUTO RNG label turns magenta (Figure 5-8).
5.1.4. Map Declutter Declutter Range Display There are four map feature declutter levels available that work in conjunction with the High (H) map range to aid in map declutter. Each level is represented by a graphical bar below the numerical range display (Figure 5-9). Med-High (MH) Change the Map Feature Declutter Level Med-Low (ML)
5.1.5.1. Invalid GPS If the aircraft GPS position data is no longer available or becomes invalid: Figure 5-10 • The associated flight plan and basemap data are retained and displayed as long as Other Valid GPS Reversion Mode aircraft position information is provided from the selected GPS. • The flight plan and waypoints become inactive and are displayed in white.
5.1.6. Airport/VOR Information CAUTION The Navigation Map provides detailed information about airports and VORs that are When the aircraft position is unavailable, the ownship shown on the display. The lower left button is labeled INFO and when pressed, the symbol is removed from the Navigation Map VIEW, EFD1000/500 MFD displays a label for the selected airport or VOR (Figure 5-13).
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Figure 5-14 Hot Key Information Displayed (if available) Figure VOR Information Page • VOR Identifier • Name and Type of VOR • Location of VOR (city, state, and country) • VOR Frequency • Bearing To and FROM VOR • Distance To VOR 5-14 • Estimated Time En route (ETE) to VOR • Latitude and Longitude to VOR...
Figure 5-17 Hot Key Information Displayed (if available) Figure Airport Communication Information Page • Selected airport’s frequencies and callsigns 5-17 • Airport Identifier • Name of Airport • Runway 5-18 • Runway Lengths and Widths • Runway Surface Type • Type of Runway Lighting • Selected airport’s METAR and TAF information 5-19 (displayed as described in Section 5.2.3.
View Airport/VOR Information NOTE With the Navigation Map VIEW selected (magenta border), press the lower Left Button labeled INFO. The Left Knob label changes to Apt/Vor and both On rare occassions when the EFD1000/500 is using the the Left Knob and Left Button label turn magenta. backup battery, the ON BAT annunciation may obscure Press the Left Knob to display the selected airport’s or VOR’s pop-up the airport information when the display is using PAGE...
5.1.8. Map Styles The Navigation Map basemap is displayed as either an IFR (Figure 5-21) or VFR Figure 5-21 Navigation Map VIEW with (Figure 5-22) style map. The map data source for the Navigation Map VIEW is the IFR Map Style Selected Jeppesen Database saved on the micro SD Card.
5.1.9. Overlays Figure 5-23 Navigation Map VIEW Overlay Hot Keys, All There are several additional map features that can be displayed on the Navigation Map Overlays Disabled VIEW, Airways, Relative Terrain, Stormscope® WX-500, Data Link Weather, and Traffic. Each of these overlays is enabled or disabled via Hot Keys (Figure 5-23). 5.1.9.1.
5.1.9.2. Terrain Overlay NOTE The Terrain Hot Key enables terrain and obstruction display as an overlay on the Navigation Map. When enabled terrain and obstructions display as outlined in For detailed information about Traffic, Stormscope® Section 5.3.1. Terrain and Obstructions and the TERR annunciation displays above WX-500, and Terrain/Obstructions see Section 5.3.
5.1.9.3. Lightning Overlay Figure 5-26 The LTNG Hot Key is a three position Hot Key that permits display of satellite lightning Lightning Overlay On information or WX 500 Spherics data overlaid on the Navigation Map VIEW. When Displaying WX-500 Cell Data enabled, the Lightning overlay displays lightning as defined in Section 5.2.
5.1.9.4. Data Link Weather Overlay Figure 5-27 Data Link Weather Overlay On The Data Link Weather Hot Key enables the display of NEXRAD and precipitation data overlaid on the Navigation Map VIEW. Coverage is limited to the US, Puerto Rico, and Canada.
5.1.9.5. Traffic Overlay NOTE The Traffic Hot Key enables the traffic display overlaid on the Navigation Map VIEW. When enabled, the Traffic overlay displays traffic threats as defined in Section 5.3.2. The Traffic overlay requires configuration with an Traffic, is oriented to the underlying Navigation Map using the normal altitude filter. appropriate traffic sensor and displays traffic using the The Hot Key label TRFC is green when enabled and gray when disabled.
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If your traffic interface is a TIS interface and traffic data is: NOTE • Unavailable the traffic label displays TRFC UNVL • Not refreshed within 6 seconds the traffic label displays TRFC COAST When GPS position or heading is invalid or unavailable the TRFC annunciation displays with a red horizontal • Not refreshed within 12 seconds the traffic label displays TRFC RMVD, and traffic line through the center of the text and traffic symbols...
5.2. Data Link Weather (optional) Data Link Weather provides graphical and textual descriptions of weather-related information received from XM WX Satellite Weather through the Aspen satellite receiver (Model EWR50) for the continental United States, Puerto Rico, and parts of Canada and Mexico.
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Each Data Link Weather product screen displays the ownship symbol and flight plan overlaid on a black background, oriented North-Up, centered in a 360° range ring. The available map ranges are the same as the Navigation Map, starting at 10 nm, with the default display at 200 nm.
5.2.1. Selecting Data Link Weather Products Figure 5-31 Data Link Weather VIEW Selected The Data Link Weather VIEW offers several types of weather product information, each displayed in a different screen of the Data Link Weather VIEW. There is a screen for each of the following Data Link Weather VIEW options: • Convection (NEXRAD, Lighting, Convective) • METARs...
5.2.2. Convective NOTE The EFD1000/500 MFD provides the pilot with several methods to view severe weather. Areas without radar coverage will display as a gray On the Navigation Map VIEW, as previously discussed, severe weather is presented as an overlay. The Convective weather product screen presents severe weather information as overlay when the NXRD Hot Key is enabled.
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Figure 5-33 The Convective screen displays severe weather information overlaid on a basic weather Convective Screen map. Precipitation is displayed as a color coded NEXRAD radar overlay on the basic weather map. The LGND Hot Key displays a legend for the precipitation coloring. Satellite lightning is displayed as cyan colored lightning symbols on top of the NEXRAD radar information.
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NEXRAD weather surveillance can detect most precipitation within 80 nm, and intense rain or snow within 140 nm, of the radar. NEXRAD measures moisture in DBz or decibels of Z, with Z representing the reflection back to the radar. NEXRAD does not report precipitation below 10 DBz.
Display the Convective Legend Figure 5-35 Convective Legend • With the Convective weather product screen displayed, press the LGND Hot Key. The Convective legend displays on the right of the screen (Figure 5-35). Hide the Convective Legend • Press the LGND Hot Key to hide the Convective legend. Hide or Display Convective Overlays •...
5.2.3. METAR The METAR screen displays graphical Aviation Routine Weather Reports with a color coded flag at weather reporting airports. A METAR is an hourly Aviation Routine Weather Report from the reporting airport (not all airports have a forecast). METARs issued in the U.S.
Display the METAR Legend Figure 5-40 METAR Flag Legend • With the METAR weather product screen displayed, press the LGND Hot Key. The METAR legend displays on the right of the screen (Figure 5-40). Hide the METAR Legend • Press the LGND Hot Key to hide the METAR legend. The pilot can display full textual details for any METAR.
Display Multiple Airports’ METAR Information Figure 5-41 Selecting a With the METAR weather product screen displayed, press the lower Left METAR to Display Button labeled INFO. The Left Knob label changes to APT and both the Left Knob and Left Button label turn magenta. Rotate the Left Knob to scroll through each METAR reporting airport.
Display an Individual Airport’s METAR Information Figure 5-43 METAR Text Edit Pop-up Window With the METAR weather product screen displayed, press the TEXT Hot Key. The METAR pop-up displays with a four character pilot-selectable airport identifier field. The first character placeholder is selected indicated by the magenta color (Figure 5-43).
5.2.4. Echo Tops The Echo Tops screen displays a graphical representation of the radar indicated top of an area of precipitation, the precipitation echo, as derived from NEXRAD information. Echo tops are displayed overlaid on a basic weather map (Figure 5-46). Figure 5-46 Echo Tops Screen The display shows the location and elevation (above MSL) of the highest radar echo.
The Echo Tops screen has an altitude filter, controlled by the Hot Keys, allowing the pilot to set the altitude for echo top display. Only echo tops at or above the selected altitude filter value will display. The pilot adjusts the altitude filter value by pressing either the FL + or the FL- Hot Key.
5.2.5. Cloud Tops The Cloud Tops screen displays a Cloud Top graphical depiction. Cloud Tops are the given height of convective and upper-level clouds determined from satellite mosaic. The Cloud Tops screen displays the graphical cloud images overlaid on the basic weather map (Figure 5-48).
Figure 5-50 5.2.6. AIRMET/SIGMET AIRMET/SIGMET The AIRMET/SIGMET screen displays a graphical depiction of AIRMETs (AIRman’s METeorological Information) and SIGMETs (SIGnificant METeorological Information). AIRMETs and SIGMETs are weather advisories broadcast by National Weather Service for the lower 48 states and adjacent coastal waters. Both AIRMETs and SIGMETs warn pilots of potentially hazardous weather.
The Hot Keys provided allow the pilot to enable and disable AIRMETs and/or SIGMETs to aid in declutter. There is a Hot Key for each type of AIRMET/SIGMET as outlined in Table 5-10. Each type of AIRMET/SIGMET will display outlined in the color indicated with a symbol centered in the outlined area affected by the AIRMET/SIGMET.
Display/Hide the AIRMET/SIGMET Legend Figure 5-51 AIRMET/SIGMET Legend • With the AIRMET/SIGMET weather product screen displayed, press the LGND Hot Key. A legend displays. Press the LGND Hot Key again to hide the legend (Figure 5-51). Display AIRMET/SIGMET • With the AIRMET/SIGMET screen displayed and selected, press any of the Hot Keys to display or hide the applicable overlay (Figure 5-52 – 5-55).
The pilot can display full textual details for any AIRMET/SIGMET. First selection mode must be activated on by pressing the lower left Detail button. Next select the particular NOTE AIRMET/SIGMET you want to read, then press the Left Knob labeled INFO to view the AIRMET/SIGMET.
5.2.7. TFR The TFR screen displays a graphical depiction of Temporary Flight Restrictions, outlined Figure 5-59 TFR in red, on a basic weather map (Figure 5-59). These restrictions are usually issued in the United States and are typically short term. They can include major sporting events, air shows, natural disaster areas, space launches, and Presidential movements.
Display TFR Information Figure 5-60 TFR Selected With the TFR weather product screen displayed, press the lower Left Button labeled INFO. The Left Knob label changes to TFR and both the Left Knob and Left Button label turn magenta (Figure 5-60). Rotate the Left Knob to select the desired TFR.
5.2.8. Winds Aloft Figure 5-63 Winds Aloft Screen at 500 nm The Winds Aloft screen displays the forecast wind speed and direction at the selected altitude above MSL on a basic weather map (Figure 5-63). Winds are depicted as barbs up to a map range of 500 nm;...
Display the Winds Aloft Legend Figure 5-65 Winds Aloft Legend • With the Winds Aloft weather product screen displayed, press the LGND Hot Key. The Winds Aloft legend displays on the right of the screen. Hide the Winds Aloft Legend •...
5.2.9. XM Status The XM Status screen displays the status of the XM weather receiver (Figure 5-66). The Figure 5-66 XM Status status includes the XM serial number (eight digit alpha numeric number), Signal Quality, Status Message, Control State, Time, and descriptive messages. The following tables provide a description of the different messages that may display for Signal Quality (Table 5-11), Status Message (Table 5-12), and Control State (Table 5-13).
5.2.9.2. Status Message Message Description Activation Required The XM receiver is indicating that the receiver is not activated. Follow the instructions to activate the receiver. Antenna Failure The XM receiver is reporting that no antenna is connected. Data Unavailable The receiver has tuned to the satellite, but data is not available (such as: off the air, weak signal condition, or service blocked for some reason).
5.2.9.3. Control States Message Description Configuring The XM unit is being configured to send certain periodic messages (such as signal quality and time) Listening Only The EFD is in listen only mode, which means that a different EFD is controlling the XM receiver, but this unit will still display any weather product that is received.
5.2.9.4. Descriptive Messages Two types of descriptive messages may be displayed, operational and error messages. Only one message will display at a time, with error messages taking precedence over operational messages. Error messages are displayed when the XM receiver becomes non-operational.
Message Description XM receiver is not communicating Communication The XM receiver is with the EFD, check power and Error not communicating connections with the EFD. Figure 5-67 XM Receiver is not receiving Antenna Error The antenna status is XM Status Product Ages Screen satellite data.
The age annunciation on each weather page indicates the elapsed time, in minutes, since the information was generated. Each weather product has an age limit and is usually updated at the Update Rate indicated in Table 5-16. Weather Product Expiration Time Update Frequency US NEXRAD Puerto Rico NEXRAD...
The data age (except Puerto Rico NEXRAD) will display in black text on an amber background if the XM receiver is not operational for 30 seconds after an error is detected. When the Expiration time has been reached, and no updates have been received, the age annunciation will display with a red slash and all data is removed from the display.
5.3. Dedicated Hazard Awareness Views The EFD1000/500 MFD Dedicated Hazard Awareness Views provide advisory information of potential hazards to flight safety associated with Terrain, Traffic, and Weather. The EFD1000/500 MFD offers three VIEWS that are dedicated solely to hazard awareness: • Terrain • Traffic • Stormscope®...
5.3.1. Terrain and Obstructions Figure 5-69 Terrain VIEW Showing an ARC Range Ring Relative terrain is displayed on a black background, with a 360° or ARC range ring, and is overlayed by the current flight plan if available. The displayable range is 5 – 100 nm with a default display of 15 nm (Figure 5-69).
Terrain data color coding and display is based on the difference between the terrain height (MSL) and the aircraft height (MSL) as shown in Table 5-18. The relative terrain CAUTION height is determined by computing the altitude difference between the terrain height Correct barometric pressure is essential to accurate and the computed Baro Corrected Altitude.
When a GPS source’s position data are invalid or no longer available, an amber annunciation, GPS1, GPS2, or RSM GPS, is shown to the left of the lower display to Figure 5-70 indicate which has failed (Figure 5-70). If Basemap features are invalid or unavailable all Invalid or Failed GPS Annunciations features except the flight plan are removed from the display.
5.3.2. Traffic (optional) Figure 5-71 Dedicated Hazard Awareness – Traffic When the EFD1000/500 MFD is configured with one of the following traffic sensors the EFD1000/500 MFD can display traffic information. The map is oriented North-Up on a black background (Figure 5-71). • Avidyne TAS 600/610/620 (TAS) • Bendix/King KMH 880 (TAS) • Bendix/King KTA 870 (TAS)
5.3.2.1. Traffic Display The Traffic VIEW is oriented Heading-Up, with either a 360° or ARC compass view, with a white outer and inner range ring. The pilot selects the compass view by pressing the 360/ARC Hot Key; 360° is the default when not previously set. The range is pilot- selectable with the outer-range ring and inner-range ring representing the following range selections from the ownship position: • 2 nm outer-range ring...
The EFD1000/500 MFD will display intruders prioritized in the order received from the Figure 5-73 Traffic Symbols configured traffic sensor. The EFD1000/500 MFD includes three threat levels using TCAS symbology; traffic advisory (amber circle), proximity advisory (cyan diamond), and other traffic (hollow cyan diamond).
For example, the intruder shown in Figure 5-74 is a Traffic Advisory 400 feet above the NOTE ownship and is descending. No altitude information is shown in the intruder data block when the altitude is unavailable. If an intruder is flying level no arrow is shown. If the intruder is not reporting altitude, neither the arrow or 5.3.2.1.2.
5.3.2.1.4. Traffic Operational Modes There are four possible modes for TAS traffic sensor status: • Operational • Standby • Test • Failure Traffic symbols are removed from the display and the EFD1000/500 MFD displays an annunciation when your traffic sensor is operating in any mode other than operational as outlined in Table 5-20.
TIS traffic is usually displayed in real time. If for some reason the traffic sensor information has not been refreshed for 6 seconds the EFD1000/500 MFD will display an age indicator and an a TRFC COAST annunciation. After 12 seconds of no updates, the EFD1000/500 MFD will continue to display the age indicator and the annunciation will change to TRFC RMVD.
The pilot adjusts the altitude filter value by pressing the ABV/BLW/NRM/UNR Hot Key, Figure 5-76 Traffic Advisory which cycles through each of the filter levels. Change the Traffic Altitude Filter • Press the ABV/BLW/NRM/UNR Hot Key to select the desired altitude filter. 5.3.2.2.
5.3.3. WX-500 (optional) Figure 5-78 WX-500 VIEW in Strike Mode When configured with a WX-500 receiver the EFD1000/500 MFD displays Stormscope® WX 500 data, oriented Heading-Up. The default display shows the 360° view, with a 200 nm range ring on a black background (Figure 5-78). The WX-500 VIEW supports an ARC or 360°...
Display WX-500 Strikes NOTE • Press the STRK/CELL Hot Key until the Hot Key label displays STRK, in green text. A STRK label displays in the upper right corner of the display and the Refer to the Stormscope® WX-500 User Guide for current strike rate displays lower right corner.
5.3.3.1. WX-500 Annunciations WX-500 data is removed from the display, the rate annunciation displays with a horizontal red line, and the ownship symbol is removed from the display when any of the following situations occur (Table 5-23). Error Message Explanation TEST INIT Sensor is in self-test mode.
5.4. Secondary Views (EFD1000 MFD only) NOTE The Secondary Attitude Instrument and Secondary HSI VIEWs are only available with the Aircraft with an EFD500 MFD configured with an EFD1000 MFD. The Horizontal Situation Indicator VIEW is available when the EFD1000/ EFD1000 PFD will not receive heading information if MFD is configured with a GPS.
When altitude, attitude or airspeed ADAHRS is invalid or unavailable the ADAHRS FAIL message displays in amber on the lower right of the data bar (Figure 5-86). Figure 5-86 When a cross check attitude condition occurs in the EFD1000 MFD the CHECK AHRS ADAHRS FAIL message displays in amber on the lower right of the data bar (Figure 5-87).
5.4.2. Secondary Horizontal Situation Indicator (HSI) Figure 5-88 Secondary HSI The Secondary HSI VIEW provides a secondary display of the Direction Indicator and Course Direction Indicator (CDI). The Secondary HSI displays on a black background with a 360° compass, the ownship symbol, and digital display of aircraft direction of flight on the bottom WINDOW of the split screen LAYOUT (PAGE 2/3) (Figure 5-88).
5.4.2.1. Vertical Deviation Indicator (VDI) Figure 5-90 Secondary HSI The secondary HSI displays the VDI scale and diamond only when a vertical deviation Displaying the VDI signal is available (Figure 5-90). The VDI scale and symbol (diamond) display to the left of the direction indicator when: • A VHF navigation radio is selected as the CDI Navigation source, the radio is in ILS mode, and is receiving valid localizer and glide slope data.
Chapter 6 Expanded Emergency & Abnormal Procedures This section supplements and provides an expanded description of the emergency and abnormal procedures included in the FAA approved Aircraft Flight Manual Supplement. The data provided here is intended to provide additional background information to enhance the pilot’s understanding of the emergency and abnormal conditions, and the associated procedures provided in the AFMS.
Indication of an obstructed pitot system is provided for EFD1000s when configured as CAUTION a PFD, a MFD, and MFD in reversionary mode. If the EFD1000’s indicated airspeed is less than 30 KIAS (35 mph) and GPS groundspeed is > 50 kts (58 mph), then attitude and Most light aircraft have only a single pitot and static heading instruments are replaced with red “X”s and textual annunciations to indicate pneumatic system available for flight instrument...
6.3. Abnormal Shutdown Procedure In the event of an EFD malfunction requiring in-flight shut down of the equipment, proceed as follows Abnormal Shutdown Procedure NOTE EFD1000 MFD (with EBB) EFD Circuit Breaker / Switch ......OFF / PULL Each EFD1000/500 has a dedicated circuit breaker EBB Disconnect Switch........DISC and master switch or combined circuit breaker switch.
6.4. MFD Reversionary Mode Operation (EFD1000 Figure 6-2 The EFD1000 MFD is on the MFD only) Right of a Three-Display Setup Select REV Mode EFD1000 MFD REV Button ........MOMENTARY PRESS REVERSIONARY PFD Display ......Configure as desired BARO SETTING ............Verify In the unlikely event of a failure of the PFD, including the loss of ADC or ADAHRS functions, the EFD1000 MFD (Figure 6-2) can revert to PFD operation.
6.5. Loss of or Degraded Aircraft Power or ON BAT Annunciation In the event that aircraft generated power to the EFD is degraded or fails, each EFD will Figure 6-3 automatically switch to its own dedicated battery (Figure 6-3). When continued safe Internal Battery Operational operation depends on the EFD1000, UNRESTORABLE LOSS OF EXTERNAL POWER IS AN EMERGENCY SITUATION.
6.6. GPSS Operation, Annunciations, and Autopilot Figure 6-4 Operating in GPSS Mode Modes GPSS is available from the EFD1000 PFD. Three modes, Enabled, Wings Level, and Disabled, are possible and annunciated in the EFD’s lower display. When enabled, the configured GPS source not only provides the basemap and flight plan data in the lower display, but also provides GPSS as the heading input to a configured autopilot.
When GPSS Automatically Changes to Wings Level Mode Figure 6-6 GPSS Disabled Check the configured GPS source. Check the EFD1000 navigation source select. If selected GPSS source is restored or changed and GPSS is still desired, press the “GPSS” Hot Key to activate GPSS (GPSS Hot Key label turns green). Disable GPSS Press the GPSS Hot Key until the Hot Key label is gray (Figure 6-6).
6.7. EBB Disconnect (EFD1000 MFD only) To isolate the EBB in the event of an EBB or EFD1000 MFD malfunction, proceed as follows: Isolate the Emergency backup battery EBB Switch ..............Select DISC NOTE The EBB is protected by thermal and short-circuit sensing circuitry to prevent battery overheating or damage.
6.8. Power Override Figure 6-7 External Power Voltage Status In the event that the pilot wishes to override the automatic power configuration of the equipment, proceed as follows: Power Override MENU................“POWER SETTINGS” Page To switch FROM aircraft power to Battery: “BATTERY”...
6.9. ADAHRS Attitude Disagreement Should differences be observed between one or more EFD1000 displays and/or the CAUTION standby instruments, monitor all available attitude, airspeed, and altitude information to diagnose faulty indicator(s). Reset the EFD1000 ADAHRS. The EFD1000 PFD and MFD may share a common pitot/static system and their otherwise independent 6.10.
Reset EFD1000 ADAHRS ATTITUDE ..............MAINTAIN STRAIGHT AND LEVEL FLIGHT by visual reference, or by standby instruments AUTOPILOT ..............DISCONNECT MENU................Select GENERAL SETTINGS A page Figure 6-11 ADAHRS: RESET?”LINE SELECT KEY ....PRESS (Figure 6-11) Main Menu GENERAL ADAHRS: RESET? LINE SELECT KEY ....PRESS AGAIN TO CONFIRM ADAHRS SETTINGS Page RESET (Figure 6-12) Activate any other control to cancel the reset...
6.11. EFD1000/500 Intercommunications Failure In the event of a “CROSS LINK FAILURE” message, verify that barometric altimeter setting CAUTION information is correctly transferred between the displays. On the EFD1000 MFD, the barometric altimeter setting can only be set from the MFD REV mode. Relative terrain is based on the barometric altitude from the EFD1000 displays.
6.12. Loss of GPS information Position and flight plan data for the PFD and MFD is provided from aircraft GPS equipment. The EFD displays may be configured to receive data from one or two CAUTION external GPS systems. In addition, when an RSM connected to the EFD includes an In the event of complete GPS failure, the Nav Map emergency GPS, this information may be used if the aircraft GPS system(s) fail.
6.13. MFD Database Card Each EFD1000 MFD and EFD500 MFD includes a microSDHC (SD card, High Capacity) card slot into which a database card with terrain and Nav Map data may be inserted. The database card must remain in the EFD display as data is dynamically loaded from the microSDHC into the EFD memory during flight as the aircraft position changes.
6.14. Warning, Caution, and Advisory Summary Applicability WARNINGS 1000 1000 (REV) Presented when the EFD is operating on the internal or Emergency Backup Battery (EBB) (as configured). The countdo replaced by the ON BAT annunciation with the battery’s % charge remaining. NOTE Figure 6-13 Battery Countdown Figure 6-14 Battery Operational...
Applicability WARNINGS 1000 1000 (REV) Red chevrons displayed on the Attitude Indicator’s pitch scale to indicate extreme pitch up and down attitudes and direction to restore level flight. Figure 6-17 Extreme Pitch Up Figure 6-18 Extreme Pitch Down Table 6-1 Warning Annunciations Page 6-16 EFD1000/500 MFD Pilot’s Guide 091-00006-001 REV B...
Applicability CAUTION 1000 1000 (REV) Presented when the EFD1000 AHRS internal integrity monitor determines that attitude is potentially degraded. If a CROSS CHECK ATTITUDE annunciation is provided the pilot should cross check attitude, airspeed and altitude indications. Figure 6-19 Cross Check Attitude Amber annunciation displayed in the data bar of the EFD1000 MFD when its internal ADAHRS reports a failure (e.g.
Applicability CAUTION 1000 1000 (REV) Annunciation accompanies an ATTITUDE FAIL, presented when indicated airspeed is less than 30 KIAS (35 mph) and GPS groundspeed is greater than 50 kts (58 mph). This provides an indication of a potentially obstructed pitot system.
Applicability CAUTION 1000 1000 (REV) Presented in the center of the NAV Map when all GPS sources have failed. When presented, the map changes to a North-up orientation and the map no longer moves with the aircraft. Manual panning is still possible and all map features that are not GPS position dependent continue to remain available, including relative terrain overlays.
Applicability CAUTION 1000 1000 (REV) Presented to indicate the aircraft is reaching (steady) or deviating (flashing) from the preselected altitude. May be accompanied by an optional one- second steady tone. Figure 6-31 Altitude Caution Presented when a connected radio altimeter indicates it has reached the altitude set by the pilot.
Applicability CAUTION 1000 1000 (REV) Presented when the previously enabled and valid GPSS source is lost or has changed. Figure 6-33 GPSS Source Lost/Changed Presented if GPS position or track is invalid or not available, altitude is invalid, or heading is invalid. Figure 6-34 Terrain Fail 091-00006-001 REV B EFD1000/500 MFD Pilot’s Guide...
Applicability CAUTION 1000 1000 (REV) Presented when a Traffic Advisory is indicated and a dedicated traffic view is not currently displayed. Push the “TRFC” prompts the pilot to select lower, middle button to view a dedicated traffic display. Figure 6-35 Traffic Advisory Page 6-22 EFD1000/500 MFD Pilot’s Guide 091-00006-001 REV B...
Applicability CAUTION 1000 1000 (REV) Presented when TIS data is unavailable. Figure 6-36 TIS Traffic Figure 6-37 TIS Traffic Unavailable Unavailable Presented when that indicates traffic data has not been refreshed within 6 seconds. Figure 6-38 Traffic Removed Presented that indicates a traffic sensor failure. Figure 6-39 Traffic Sensor Failure Presented that indicates that the link between the EFD and traffic has been lost (e.g., traffic sensor is OFF).
Applicability CAUTION 1000 1000 (REV) Presented when a lightning (spherics) sensor self-test report is not been received within 10 seconds. Figure 6-41 WX-500 Self Test Failure Presented for a failed lightning (spherics) sensor self-test or sensor status is a fatal fault or undefined. Figure 6-42 WX-500 Self Test Failure Presented when the lightning (spherics) sensor has an undefined recoverable error...
Applicability CAUTION 1000 1000 (REV) Presented when the lightning (spherics) sensor has a recoverable inhibit line stuck microphone error Figure 6-45 WX-500 Inhibit Line Error Presented when the lightning (spherics) sensor has a recoverable changed antenna jumper error. Figure 6-46 WX-500 Antenna Jumped Error Presented when the lightning (spherics) sensor has lost heading reference and, therefore, a removal of lightning (spherics) sensor data.
Applicability CAUTION 1000 1000 (REV) Datalink weather product data not received for 30 seconds after an error is detected. NOTE Figure 6-49 Datalink Weather Data Error Some weather product pages have a different label. Figure 6-50 Free Gyro Mode Figure 6-51 Battery Failed Table 6-2 Caution Annunciations Page 6-26 EFD1000/500 MFD Pilot’s Guide...
Applicability ADVISORY 1000 1000 (REV) Presented when the EFD500 MFD’s “REV” button is pressed. Figure 6-52 REV Button Off Presented when the EFD1000 MFD’s “REV” button is pressed and held when operating as a MFD. Figure 6-53 REV Button Off Presented when GPSS is enabled and the GPS source is valid.
Applicability ADVISORY 1000 1000 (REV) Associated with the GPS coupled to the HSI or Secondary HSI. See the GPS AFMS for more information. Figure 6-55 GPS Annunciations Indicates the traffic sensor is enabled Figure 6-56 Traffic Enabled Indicates the traffic sensor is in standby. Figure 6-57 Traffic Sensor Standby Indicates the traffic sensor is in the self-test mode.
Applicability ADVISORY 1000 1000 (REV) Indicates the traffic data has not been refreshed within 6 seconds. Figure 6-59 Traffic Data Older Than Six Seconds Lightning (spherics) Strike display mode selected. The rate indicates the approximate number of lightning strikes detected per minute. Figure 6-60 WX-500 Strike Rate Lightning (spherics) Cell clustering display mode selected.
Applicability ADVISORY 1000 1000 (REV) Data age presented for all Data Link Weather products when the XM receiver is operational. Elapsed time is expressed in minutes (e.g., :05). NOTE Figure 6-64 Datalink Weather Product Data Age Some weather product pages have a different label. A horizontal red line through any legend indicates that the data is invalid or unavailable.
Applicability ADVISORY 1000 1000 (REV) Annunciation presented at the bottom center of the Nav Map if the software is unable to access the data base stored to the microSDHC memory card Figure 6-68 Database Failure Annunciation presented at the bottom center of the Nav Map when data is being loaded from the micro SD card at start up.
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This Page Intentionally Left Blank Page 6-32 EFD1000/500 MFD Pilot’s Guide 091-00006-001 REV B...
SRTM Shuttle Radar Topography Mission terrain database. If this is your first visit to the Aspen Avionics Customer Port, click the Register button Table 7-1 Jeppesen Data Types on the login screen to register all your Aspen products and gain access to the Aspen Customer Port.
> Support > Technical Support For questions about Customer accounts, username/passwords, other Jeppesen products and services contact Jeppesen Customer Service. 800-621-5377 or 303-799-9090 captain@jeppesen.com For questions about Evolution Flight Display functionality, contact Aspen Avionics. salessupport@aspenavionics.com 505-856-5034 Page 7-2 EFD1000/500 MFD Pilot’s Guide...
7.2. XM Weather Receiver Activation An Evolution Weather Receiver (or equivalent) and subscription to XM WX Satellite Radio Service is required for display of the EFD1000/500 MFD Weather Products. If the EFD1000/500 MFD is installed with a weather receiver, when the EFD1000/500 MFD is turned on for the first time an annunciation will display alerting you that the XM WX Satellite Radio Service is not yet activated.
7.3. Specifications Input Voltage +8 to +32 Volts DC 7.3.1. EFD Display Unit Max Current 2.4 Amps @ 28 VDC 4.8 Amps @ 14 VDC GENERAL SPECIFICATIONS: I/O SPECIFICATIONS: Width 3.50 in. (Measured at Bezel) ARINC 429 Inputs Height 7.00 in. (Measured at Bezel) ARINC 429 Outputs Can Depth 4.15 in.
7.3.2. Remote Sensor Module (RSM) 7.3.4. Operational Width 2.65 in. Airspeed Range Minimum displayed airspeed 20 KIAS Length 4.40 in Maximum displayed airspeed 999 KIAS Height 1.00 in. Altitude Range Minimum displayed altitude -1,500 ft MSL Maximum displayed altitude 60,000 ft MSL Weight 0.2 lbs Vertical Speed...
7.3.5. Emergency Backup Battery Width 3.6 in. (Widest Point on Mounting Clips) Height 1.7 in. Length 8.52 in. (Rear of Mounting Tray to Connector) Weight 2.25 lbs (with Mounting Bracket) Operating Temp -20°C to +55°C Storage Temp -55°C to +85°C Max Un-Pressurized Operating Altitude 35,000 ft Max Pressurized Operating Altitude...
VIEW as the primary reference for navigation. The EFD1000/500 MFD Navigation VIEW is intended to be a supplement to other approved aspects of this Pilot’ s Guide. Aspen Avionics highly recommends learning navigation data sources, and enhance the pilot’ s overall situational how to operate the EFD1000/500 MFD on the ground and under VFR conditions to become completely familiar with the product.
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There are no pilot-serviceable parts on the EFD1000/500 MFD. Only and advisory in nature, and therefore cannot be relied upon as safety- Aspen Avionics Authorized Dealers can make repairs on the EFD1000/500 critical in connection with any aircraft or other usage. XM is not MFD.
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CAUTION NOTE The EFD1000/500 MFD displays use an LCD display that is susceptible to Consult all Aircraft Flight Manual Supplements (AFMS) provided by the scratches, skin oils, and abrasive cleaners. Do not use cleaners containing aircraft manufacturer and/or installed sensors prior to operation of the ammonia (window cleaners).
7.5. Symbology Figure 7-3 Figure 7-2 Airports Navaids Airport Symbols NAVAID Symbols Control Tower Active Waypoint No Control Tower Active Leg Other Waypoint Figure 7-4 Airways Airway Symbols Other Leg VORTAC or VOR/DME Figure 7-5 Declutter Declutter Symbols DME or TACAN High Med-High Med-Low...
7.6. Glossary Back Course Localizer back course approach where the signal on the back side of the localizer is used Accuracy Estimated position accuracy in feet or meters. for alignment to the runway opposite of normal localizer alignment. Without compensation the Analog to Digital CDI would reverse sense.
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Course Enroute Safe Altitude The recommended minimum altitude within ten miles left or right of the desired course on Course to Steer an active flight plan. decibels ‘Z’ (radar return) ETA (Destination) Estimated Time of Arrival. The estimated time Direct Current you will reach a Go To destination, or the final waypoint in a route.
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Global Positioning System KIAS Knots Indicated Air Speed GPSS GPS Steering kilometer Ground Track see Track Knots Groundspeed The velocity that the aircraft is travelling relative Latitude to a ground position. Liquid Crystal Display Glide Slope or Ground Speed Lateral Deviation Indicator Heading The direction an aircraft is pointed, based upon The portion of a flight plan between two...
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NRST Nearest TRSA Terminal Radar Service Area Outside Air Temperature Volts, alternating current Omni-Bearing Selector Volts, direct current ºC Degrees Celsius Vertical Deviation Indicator ºF Degrees Fahrenheit Visual Flight Rules Primary Flight Display Very High Frequency Radio Magnetic Indicator VLOC VOR/Localizer Remote Sensor Module VHF Omni-Directional Radio Range...
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Deactivate ..........................5-12 GPS POS Failed ........................6-19 Turn Off or On ........................5-12 GPS Reversion ........................6-18 GPS Reversion Emergency Use Only ..............6-18 GPSS Source Lost/Changed ..................6-21 Minimums Caution ......................6-19 Backup Battery .........................4-16 RSM GPS ...........................6-18 Emergency (EBB) ........................4-16 Terrain Fail ..........................6-21 Internal............................4-16 TIS Traffic Unavailable ......................6-23 Internal Housing Temperature ...................4-17 Traffic Advisory ........................6-22...
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Configuring ..........................5-50 Expiration Date ......................4-2, 4-3 Controlled Airspace, Feature Group................5-4 Validity ............................4-2 Controls ..........................3-8–3-11 Validity and Expiration Dates, View ................4-3 Hot Keys ...........................3-11 Database Failure ........................6-31 Left Button ..........................3-9 DATABASE FAILURE ........................5-4 Left Knob ............................3-8 Data Invalid or Unavailable ....................6-30 Menu Button .........................3-11 Data Link Weather .....................5-26–5-55 Menu Keys ..........................3-11...
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Datalink Weather Product Data Age ................6-30 EFD500 Display ...........................1-6 Data Link Weather Products, Selecting ..............5-28 EFD1000 Display ........................1-5 Data Link Weather Products, View Different ............5-28 EFD Display Unit .........................7-4 Data Unavailable ........................5-49 Emergency Backup Battery ....................7-6 Decision Height Caution ....................6-20 Emergency Backup Battery, Isolate ................6-8 Declutter ..........................5-3, 5-13 Emergency GPS ..........................1-4...
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MFD Reversionary Mode Operation .................6-4 GPS Navigation Source, Change ...................5-13 ON BAT Annunciation ......................6-5 GPS POS Failed .........................6-19 Pitot/Static System Blockage ................6-1–6-2 GPS Reversion ...........................6-18 Power Override ........................6-9 GPS# REVERSION ........................5-14 WARNINGS ..........................6-15 GPS Reversion Emergency Use Only ................6-18 External Voltage Status, View .................4-18, 6-9 GPSS Off ............................6-30 Extreme Pitch Down ......................6-16 GPSS On............................6-27...
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